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Airworthiness Directives (ADs)

The aircraft owner or operator shall comply with Airworthiness Directives issued by the CAA or the aeronautics authority of the State of Design (SoD) of the aviation products, appliances and parts, and take all necessary actions thereto.

Note: Select「+」icon to explore the Applicability of AD and Click CAA AD Number to show more detailed AD information.

CAA AD Number Issue Date Aeronautics Authority of Original AD Original AD Number Applicability Download
CAA-2006-10-011A 2006/11/28 EASA 2006-0315R1 AIRBUS A330 aircraft, models -201, -202, - 203, - 223, -243, -301, -321, - 322, -323, -341, -342 and -343, all serial numbers, except those on which AIRBUS modification 49202 has been embodied in production or AIRBUS Service Bulletin (SB) A330-57-3090 has been embodied in service. AIRBUS aircraft A340-200 and A340-300 series, all certified models, all serial numbers, except those on which AIRBUS modification 49202 has been embodied in production or AIRBUS Service Bulletin (SB) A340-57- 4098 has been embodied in service. This Airworthiness Directive (AD) is not applicable to A340 200/-300 aircraft repaired in accordance with Repair Drawing R57115053 or R57115051 or R57115047 (installation of Titanium Doubler) which are covered by EASA AD 2006-0314.
CAA-2006-11-012(已有後續修訂版) 2006/11/27 Germany LBA D-2006-394 Dornier 228-212
CAA-2006-11-011 2006/11/27 FAA 2006-24-02 This AD applies to Boeing Model 747-100, 747-100B, 747-200B, 747-200C, 747-200F, 747SR, and 747SP series airplanes, certificated in any category; line numbers 001 through 430 inclusive.
CAA-2006-11-010(已有後續修訂版) 2006/11/24 EASA 2006-0350 Passenger Seats 12M( )( )-( )( )( )( )( )( ), all Part Numbers (P/N’s) as listed in Aviointeriors Service Bulletin 12M/F68-01 Revision 1 dated 2 October 2006. The affected seats are known to be installed on, but not limited to, the following aircraft: - ATR 42 series; - ATR 72 series.
CAA-2006-11-009(已有後續修訂版) 2006/11/24 ANAC 2006-09-04(BRASIL) This Emergency Airworthiness Directive is applicable to all Embraer ERJ-190( ) aircraft models in operation.
CAA-2006-10-009A 2006/11/24 EASA 2006-0309R1 A340-211, A340-212, A340-311 and A340-312 aircraft, all serial numbers, except those on which AIRBUS modification 42445 has been embodied in production or AIRBUS Service Bulletin (SB) A340-78-4031 in service. This applicability is established considering that the aircraft have not been subject to any replacement of the thrust reverser since delivery or AIRBUS SB A340-78-4031 embodiment. It is the responsibility of the operator to check that its aircraft is in compliance with the present Airworthiness Directive (AD). Reason: During a shop inspection on thrust
CAA-2006-10-003修訂(已有後續修訂版) 2006/11/24 FAA 2006-20-06 Correction This AD applies to General Electric Company (GE) CF34-10E2A1, -10E5, -10E5A1, -10E6, -10E6A1, and -10E7 turbofan engines. These engines are installed on, but not limited to, Embraer ERJ 190-100-STD, ERJ 190-100-LR, and ERJ 190-100-IGW airplanes.
CAA-2006-11-008 2006/11/23 FAA 2006-23-15 Model 757-200, -200PF, -200CB, and -300 series airplanes
CAA-2006-11-007(已有後續修訂版) 2006/11/23 ANAC 2006-11-03(BRASIL) Embraer ERJ 190 ( ) aircraft models in operation.
CAA-2006-09-011A 2006/11/17 EASA 2006-0285R1 AIRBUS 310 and A300-600 aircraft, all certified models and all serial numbers. The applicability for each of the actions required by this directive is identified in each relevant "Action" paragraph of the Compliance-section of this Airworthiness Directive (AD)
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